Abstract The possibility to synthesize the attitude control for a gyrostabilized platform is investigated under the most general assumptions on its drifts, using the principle of maximum. The analytical form of the control vector, explicitly depending on all components of the state vector of a navigation system of a descent vehicle, is a specific feature of the found solution.
Synthesis of Attitude Control for a Gyroscopic Stabilizer of the Navigation System of a Descent Vehicle
Cosmic Research ; 39 , 5
2001
Aufsatz (Zeitschrift)
Englisch
BKL: | 55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung | |
Lokalklassifikation TIB: | 770/3520/8000 |